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SHOCK-WAVE LAMINAR-BOUNDARY-LAYER INTERACTION ON A CONVEX WALL

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BookPublisher: Nasa, Washington, D.C. 1960Description: 28.DDC classification: NASA | TN D-512

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-512 (Browse shelf)	Not for loan		TR15760

Total holds: 0

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Previous	NASA TN D-5117 - OPTIMAL THREE DIMENSIONAL LAUNCH VEHICLE TRAJECTORIES WITH ATTITUDE AND ATTITUDE RATE CONSTRAINTS2	NASA TN D-5118 - RESPONSE OF AN INFINITE ELASTIC PLATE TO AXISYMMETRIC INITIAL VELOCITY DISTRIBUTIONS WITH APPLICATION TO HYPERVELOCITY IMPACT	NASA TN D-5119 - ANNEALING OF 22-, 40-,AND 158-MEV PROTON DAMAGE IN N- AND P-TYPE SILICON	NASA TN D-512 SHOCK-WAVE LAMINAR-BOUNDARY-LAYER INTERACTION ON A CONVEX WALL	NASA TN D-5120 - EFFECTS OF CLOUD COVER ON SELECTION OF RECOVERY SITES FOR FUTURE EARTH ORBITAL MISSIONS	NASA TN D-5121 - EXPERIMENTAL STAGNATION-POINT VELOCITY GRADIENTS AND HEAT-TRANSFER COEFFICIENTS FOR A FAMILY OF BLUNT BODIES AT MACH 8 AND ANGLES OF ATTACK	NASA TN D-5122 - INVESTIGATION OF PLASMA ACCELERATOR WITH MAGNETIC FIELD ARRANGED TO PRODUCE A DIVERGENT-NOZZLE EFFECT	Next

Bound With Nasa Tn D-511,513-20

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